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Experiences with the design and implementation of flutter suppression systemsResearch efforts aim at flutter suppression are discussed. The application of active controls technology to reduce the aeroelastic response of aircraft structures is discussed. Feedback control, control law design processes and synthesis, wind tunnel studies, and delta-wing wind tunnel models are discussed.
Document ID
19840012525
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Newsom, J. R. (NASA Langley Research Center Hampton, VA, United States)
Abel, I. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 11, 2013
Publication Date
March 1, 1984
Publication Information
Publication: NASA Aircraft Controls Research, 1983
Subject Category
Aircraft Stability And Control
Accession Number
84N20593
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19840012499Collected WorksNASA Aircraft Controls Research, 1983
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